Laws of life dispersion and statistical estimation of life distribution boundaries as applied to aviation engine LPC disks

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Abstract

The fatigue life variation coefficients versus its base were obtained on the basis of statistic processing of titanium disks test and operation results. The lower boundaries of the D-30 and D-30KU engines’ LPC stage 1 disk life distribution in the area of fillets of dovetailed grooves were determined.

About the authors

V. V. Kutyrev

Central Institute of aviation Motors, Moscow

Author for correspondence.
Email: vest@ssau.ru
Russian Federation

S. V. Teplova

Central Institute of aviation Motors, Moscow

Email: vest@ssau.ru
Russian Federation

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Copyright (c) 2015 VESTNIK of the Samara State Aerospace University

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